Growing community of inventors

Chandler, AZ, United States of America

Bruce David Reynolds

Average Co-Inventor Count = 3.06

ph-index = 5

The patent ph-index is calculated by counting the number of publications for which an author has been cited by other authors at least that same number of times.

Forward Citations = 74

Bruce David ReynoldsNick A Nolcheff (13 patents)Bruce David ReynoldsJohn Repp (8 patents)Bruce David ReynoldsTimothy Gentry (8 patents)Bruce David ReynoldsRichard David Conner (7 patents)Bruce David ReynoldsJohn A Gunaraj (4 patents)Bruce David ReynoldsMichael T Barton (3 patents)Bruce David ReynoldsPeter Hall (3 patents)Bruce David ReynoldsMahmoud Mansour (2 patents)Bruce David ReynoldsDavid Richard Hanson (2 patents)Bruce David ReynoldsJeffrey W Gluck (2 patents)Bruce David ReynoldsKent L Kime (1 patent)Bruce David ReynoldsRaymond Gage (1 patent)Bruce David ReynoldsBruce D Wilson (1 patent)Bruce David ReynoldsCostas Vogiatzis (1 patent)Bruce David ReynoldsTimothy Darling (1 patent)Bruce David ReynoldsTheodore Westerman (1 patent)Bruce David ReynoldsErnest Kurschat (1 patent)Bruce David ReynoldsJeffrey D Harrison (1 patent)Bruce David ReynoldsDarrell K James (1 patent)Bruce David ReynoldsSrinivas Jaya Chunduru (1 patent)Bruce David ReynoldsPei-Ching Li (1 patent)Bruce David ReynoldsRyan Bernaud (1 patent)Bruce David ReynoldsGreyson Boyll (1 patent)Bruce David ReynoldsJonathan C Bittner (1 patent)Bruce David ReynoldsBruce David Conner (0 patent)Bruce David ReynoldsJeffery W Gluck (0 patent)Bruce David ReynoldsJohn Gunaraj (0 patent)Bruce David ReynoldsMichael Todd Barton (0 patent)Bruce David ReynoldsJon Bittner (0 patent)Bruce David ReynoldsBruce David Reynolds (27 patents)Nick A NolcheffNick A Nolcheff (39 patents)John ReppJohn Repp (15 patents)Timothy GentryTimothy Gentry (8 patents)Richard David ConnerRichard David Conner (10 patents)John A GunarajJohn A Gunaraj (13 patents)Michael T BartonMichael T Barton (14 patents)Peter HallPeter Hall (7 patents)Mahmoud MansourMahmoud Mansour (10 patents)David Richard HansonDavid Richard Hanson (6 patents)Jeffrey W GluckJeffrey W Gluck (2 patents)Kent L KimeKent L Kime (11 patents)Raymond GageRaymond Gage (7 patents)Bruce D WilsonBruce D Wilson (7 patents)Costas VogiatzisCostas Vogiatzis (7 patents)Timothy DarlingTimothy Darling (4 patents)Theodore WestermanTheodore Westerman (3 patents)Ernest KurschatErnest Kurschat (2 patents)Jeffrey D HarrisonJeffrey D Harrison (2 patents)Darrell K JamesDarrell K James (2 patents)Srinivas Jaya ChunduruSrinivas Jaya Chunduru (2 patents)Pei-Ching LiPei-Ching Li (1 patent)Ryan BernaudRyan Bernaud (1 patent)Greyson BoyllGreyson Boyll (1 patent)Jonathan C BittnerJonathan C Bittner (1 patent)Bruce David ConnerBruce David Conner (0 patent)Jeffery W GluckJeffery W Gluck (0 patent)John GunarajJohn Gunaraj (0 patent)Michael Todd BartonMichael Todd Barton (0 patent)Jon BittnerJon Bittner (0 patent)
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Inventor’s number of patents
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Strength of working relationships

Company Filing History:

1. Honeywell International Inc. (26 from 15,586 patents)

2. Alliedsignal Inc. (1 from 3,002 patents)


27 patents:

1. 12286896 - System and method for turbomachine with local vortex generator array

2. 12196141 - Systems and methods with distributed bleed for gas turbine engine compressor stabilization

3. 11946474 - Gas turbine engine with compressor bleed system for combustor start assist

4. 11885234 - System and method for turbomachine with local vortex generator array

5. 11608744 - System and method for air injection passageway integration and optimization in turbomachinery

6. 11473438 - Grooved rotor casing system using additive manufacturing method

7. 11466694 - Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof

8. 11421544 - Compressor section of gas turbine engine including hybrid shroud with casing treatment and abradable section

9. 11371354 - Characteristic distribution for rotor blade of booster rotor

10. 11286779 - Characteristic distribution for rotor blade of booster rotor

11. 11156092 - Multistage axial-centrifugal compressor systems and methods for manufacture

12. 11098731 - Grooved shroud casing treatment for high pressure compressor in a turbine engine

13. 11015465 - Compressor section of gas turbine engine including shroud with serrated casing treatment

14. 11015614 - Variable vane devices containing rotationally-driven translating vane structures and methods for the production thereof

15. 10876423 - Compressor section of gas turbine engine including hybrid shroud with casing treatment and abradable section

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as of
12/6/2025
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